Alpha Titanium Alloys - an overview | ScienceDirect Topics
IMI 829 (Ti–5.6Al–3.5Sn–3Zr–1Nb–0.25Mo–0.3Si) has been derived from IMI 685 by replacing some of the Zr with the more potent strengthener Sn. It is β-heat-treated and has sufficient higher temperature capability to be used in the hotter regions of engines.
Materials for Gas Turbines An Overview - IntechOpen
2018925 · Alloy 834 (Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si-0.06C), a relatively rece nt grade, in contrast is used in D + E condition, with a 5-15% equiaxed D in the microstructure to optimize both creep and fatigue strength (Gogia, 2005). The alloy was aimed at replacing the Alloys 685 and 829 preferred in European jet engines.
Ti 6Al-4V: Ti 6Al-4V ELI: Ti-5Al-2.5Sn: Ti-3Al-2.5V: Ti 6Al-7Nb: Ti 15Mo: Ti-15Mo-3Nb-3Al-0.6Si: Ti 13V-11Cr-3Al: Ti Beta III (11.5Mo-6Zr-4.5Sn) Ti Beta C (3Al-8V-6Cr-4Mo-4Zr) Ti 15V-3Cr-3Sn-3Al: Ti 829 (5.5Al-3.5Sn
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The search phrase you entered, titanium alloy, is common to 426 materials, by searching on the exact phrase [ "titanium alloy"] in the most common text fields. Results are displayed up to a maximum of 200 materials per page. ... (Ti-5.5Al-3.5Sn-3Zr-1Nb-0.25Mo-0.3Si) 47: Titanium IMI 834: 48: Titanium 1100 Beta Quenched and annealed: 49: